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超声速混合层的光程差

Optical path difference of the supersonic mixing layer.

作者信息

Gao Qiong, Jiang Zongfu, Yi Shihe, Zhao Yuxin

机构信息

College of Photon-Electron Science and Engineering, National University of Defense Technology, Changsha, Hunan 410073, China.

出版信息

Appl Opt. 2010 Jul 1;49(19):3786-92. doi: 10.1364/AO.49.003786.

Abstract

The distorted wavefront due to the density fluctuation of the supersonic mixing layer is measured by the nano-based planar laser scattering technique, with the spatiotemporal resolutions as 10(-1) mm and 1 micros (time interval between two exposures), respectively. The optical path difference (OPD) is analyzed from the viewpoints of correlation and structure functions. Depending on the structure of the flow field, the type of the correlation function is Gaussian or exponential. The power index of the structure function is about 1.1, and the consistency over many cases is quite good. The far-field propagation of the Gaussian beam is simulated by Fourier transform, and the Strehl ratio is calculated with the rms of the OPD. The beam center and beam spread about the center in the far field are calculated, and are dominated by the statistics of the tilt of the distorted wavefront. The results indicate that aero-optical aberrations can severely limit the performance of airborne laser systems.

摘要

利用基于纳米的平面激光散射技术测量了由于超声速混合层密度波动引起的畸变波前,其空间和时间分辨率分别为10^(-1)毫米和1微秒(两次曝光之间的时间间隔)。从相关性和结构函数的角度分析了光程差(OPD)。根据流场结构,相关函数的类型为高斯型或指数型。结构函数的幂指数约为1.1,在许多情况下的一致性相当好。通过傅里叶变换模拟了高斯光束的远场传播,并利用OPD的均方根计算了斯特列尔比。计算了远场中的光束中心和围绕中心的光束扩展,它们由畸变波前倾斜的统计特性主导。结果表明,气动光学像差会严重限制机载激光系统的性能。

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